Airplane Flight Manual
Page 10
Sub-section - 4.10
NORMAL PROCEDURES
FAA Approved
Revision A3:
Apr 26, 2007
CABIN ALTITUDE SETTING FOR LANDING
(Apply setting correction to field pressure altitude)
Landing Reference Speed (V
REF
) UP TO Maximum Landing Weight
Landing Reference Speed (V
REF
)
ABOVE Maximum Landing Weight
DESCENT CHECKS
MAIN AIR VLVs 1 & 2 ..................................................OPEN
Pressurization ..............................................................Set
Briefing.........................................................................Given
NOTE: During descent, at low thrust lever settings, the fuel flow indication may become
erratic or indicate zero.
QNH - mb or HPa
970
975
980
985
990
995
1000
in Hg
28.64
28.79
28.94
29.09
29.23
29.38
29.53
Correction - ft
+1500
+1350
+1250
+1100
+950
+800
+650
QNH - mb or HPa
1005
1010
1015
1020
1025
1030
1035
in Hg
29.68
29.82
29.97
30.12
30.27
30.41
30.56
Correction - ft
+550
+400
+250
+100
0
-150
-300
Weight
17,000 lb
7711 kg
18,000 lb
8165 kg
19,000 lb
8618 kg
20,000 lb
9072 kg
V
REF
KIAS
108
111
114
118
Weight
21,000 lb
9525 kg
22,000 lb
9979 kg
23,000 lb
10,433 kg
23,350 lb
10,591 kg
V
REF
KIAS
121
123
126
127
Weight
24,000 lb
10,886 kg
25,000 lb
11,340 kg
26,000 lb
11,793 kg
27,000 lb
12,247 kg
28,000 lb
12,701 kg
V
REF
KIAS
129
131
134
136
137
Minimum Single Engine V
REF
= 111 KIAS
Icing ..................................Use V
REF
+ 10
No Flap .............................Use V
REF
+ 15
Icing/No Flap.....................Use V
REF
+ 30
For Training Purposes Only